Premium research interface

The modern interface for aviation safety intelligence.

Search investigations, review source evidence, monitor watched reports, and trace long-term patterns from one calm, data-first workspace.

63k+
Reports indexed
1940-2026
Coverage
Recent
Last data refresh
Featured Report

Loading…

Loading featured report…

Loading…
Open Report

Safety trends by operating rule

Track fatal and non-fatal accident patterns across Part 91, Part 135, and Part 121 operations.

Loading trend charts…

Browse the aviation graph

Move quickly by aircraft, airport, operator, and time with indexes built for research, not wandering.

Last Data Update

By Decade

By Month

Aircraft Manufacturer

More manufacturers

Airports

More airports

Operators

More operators

About

Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

The goal is practical safety education: make it faster to find relevant investigations, compare similar events, review factual records, and understand the evidence behind probable-cause and preliminary reports.

The investigative work and source records belong to the National Transportation Safety Board and the published investigation record. This site is not affiliated with or endorsed by the NTSB.

FAQs

NTSB Report

May 5, 1984 · Beech 35 · N2830V

Sanford, FL

Overview

Report Status
Preliminary report
Event Type
Accident
Date
May 5, 1984
Injury Outcomes
1 injury (1 serious injury)
Location
Sanford, FL
Aircraft
Beech 35
Tail Number
N2830V
Injuries
Serious
Aircraft Damage
Destroyed
NTSB Number
MIA84FA161

THE ENG LOST POWER WHEN THE ACFT WAS ON FINAL APCH TO LAND. THE PLT STATED THAT HE THEN SWITCHED FUEL TANKS, ACTIVATED THE ELECTRIC FUEL BOOST PUMP & WORKED THE RELATED WOBBLE PUMP AS FAST AS HE COULD, BUT WAS UNABLE TO RESTORE ENG POWER. SUBSEQUENTLY, THE ACFT CRASHED INTO A BUILDING AND CARTWHEELED INTO A PARKING LOT. AN EXAM OF THE WRECKAGE REVEALED THE LEFT FUEL TANK WAS EMPTY. ABOUT 10 GAL OF FUEL WAS REMAINING IN THE RIGHT TANK & AN UNDETERMINED AMOUNT OF FUEL WAS IN THE AUX TANK. THE WOBBLE PUMP/FUEL SELECTOR ASSEMBLY'S TANK SELECTOR VALVE, PN 35-924068, WAS MODIFIED, BUT WAS NOT INSTALLED IN ACCORDANCE WITH THE MANUFACTURE'S SPECIFICATION. THE SELECTOR'S DETENT BALL, PN35-921166, WAS MISSING & THE ASSEMBLY'S SPRING WAS RIDING ON THE VALVE. ALSO, THE ASSEMBLY'S HOUSING, PN 35-921185, WAS DAMAGED. IN THIS CONDITION, THE PLT COULD NOT DETERMINE THE EXACT POSITION OF THE SELECTOR VALVE. AN EXAM OF THE ACFT REVEALED IT HAD CRASHED IN A STEEP NOSE DOWN, LEFT WING LOW ATTITUDE.

Full Narrative

THE ENG LOST POWER WHEN THE ACFT WAS ON FINAL APCH TO LAND. THE PLT STATED THAT HE THEN SWITCHED FUEL TANKS, ACTIVATED THE ELECTRIC FUEL BOOST PUMP & WORKED THE RELATED WOBBLE PUMP AS FAST AS HE COULD, BUT WAS UNABLE TO RESTORE ENG POWER. SUBSEQUENTLY, THE ACFT CRASHED INTO A BUILDING AND CARTWHEELED INTO A PARKING LOT. AN EXAM OF THE WRECKAGE REVEALED THE LEFT FUEL TANK WAS EMPTY. ABOUT 10 GAL OF FUEL WAS REMAINING IN THE RIGHT TANK & AN UNDETERMINED AMOUNT OF FUEL WAS IN THE AUX TANK. THE WOBBLE PUMP/FUEL SELECTOR ASSEMBLY'S TANK SELECTOR VALVE, PN 35-924068, WAS MODIFIED, BUT WAS NOT INSTALLED IN ACCORDANCE WITH THE MANUFACTURE'S SPECIFICATION. THE SELECTOR'S DETENT BALL, PN35-921166, WAS MISSING & THE ASSEMBLY'S SPRING WAS RIDING ON THE VALVE. ALSO, THE ASSEMBLY'S HOUSING, PN 35-921185, WAS DAMAGED. IN THIS CONDITION, THE PLT COULD NOT DETERMINE THE EXACT POSITION OF THE SELECTOR VALVE. AN EXAM OF THE ACFT REVEALED IT HAD CRASHED IN A STEEP NOSE DOWN, LEFT WING LOW ATTITUDE.

Flight

Event TypeAccident
Event Time14:37 EDT
Nearest AirportSANFORD (1nm)
Runway9
Runway Length8000 ft
Runway Width150 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBeech 35
Tail NumberN2830V
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · E-185-11 · Reciprocating · 205
Seats4

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 33 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind140° @ 5 kt
Visibility7 sm
CeilingBroken clouds 3000 ft
Altimeter30.00 inHg
Observation Time18:37
Weather SourceWFAC

Appendix: Source Data